• DocumentCode
    518400
  • Title

    Notice of Retraction
    Automatic thrust augmentation

  • Author

    Balaji, S. ; Dinesh, M. ; Raj, N Dileep

  • Author_Institution
    Aeronaut. Eng. Dept., Rajalakshmi Eng. Coll., Chennai, India
  • Volume
    5
  • fYear
    2010
  • fDate
    16-18 April 2010
  • Abstract
    Notice of Retraction

    After careful and considered review of the content of this paper by a duly constituted expert committee, this paper has been found to be in violation of IEEE´s Publication Principles.

    We hereby retract the content of this paper. Reasonable effort should be made to remove all past references to this paper.

    The presenting author of this paper has the option to appeal this decision by contacting TPII@ieee.org.

    The automatic thrust augmentation is the method of powering a high speed aircraft with the objective of minimizing the fuel consumption and making use of the atmospheric air in collecting the propellant. The automatic thrust augmentation is a system that can be used in assisting the main engine in order to provide thrust during critical situations which includes crossing the sonic region, during air combat, taking off from an aircraft carrier and so on. This method of thrust augmentation includes making use of the atmospheric air in collecting the propellant (oxidizer) and mixing it with the aircraft´s fuel for the combustion to take place. Also, these processes occur automatically without pilots´ effort which also increases accuracy and relieves pilot´s stress. Since we are collecting the propellant from atmosphere, we can minimise fuel consumption significantly, and further research in this can lead to many other developments in aerospace field. We have given a conceptual idea on extracting the propellant from atmosphere and on providing automatic thrust augmentation.
  • Keywords
    aerospace engines; aerospace propulsion; aerospace field; aircraft carrier; automatic thrust augmentation; engine; high speed aircraft; Aircraft propulsion; Atmosphere; Combustion; Cryogenics; Engines; Fuels; Level control; Magnetic liquids; Oxygen; Refrigeration; minimising fuel consumption; propellant extraction from atmosphere; thrust augmentation;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Computer Engineering and Technology (ICCET), 2010 2nd International Conference on
  • Conference_Location
    Chengdu
  • Print_ISBN
    978-1-4244-6347-3
  • Type

    conf

  • DOI
    10.1109/ICCET.2010.5486136
  • Filename
    5486136